View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27855U 03034B 24282.33208385 -.00000191 00000-0 -17428-3 0 9995
2 27855 0.1326 183.5502 7136895 187.8598 41.3905 2.24663010173838
| Epoch (UTC): | 08 October 2024 07:58:12 |
| Eccentricity: | 0.7136895 |
| inclination: | 0.1326° |
| perigee height: | 672 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 183.5502° |
| argument of perigee: | 187.8598° |
| revolutions per day: | 2.24663010 |
| mean anomaly at epoch: | 41.3905° |
| orbit number at epoch: | 17383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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